View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 14212.60938943 .00000024 00000-0 60004-4 0 4322
2 24278 098.5131 220.3395 0350717 182.2160 327.2770 13.53026600886678
| Epoch (UTC): | 31 July 2014 14:37:31 |
| Eccentricity: | 0.0350717 |
| inclination: | 98.5131° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 220.3395° |
| argument of perigee: | 182.2160° |
| revolutions per day: | 13.53026600 |
| mean anomaly at epoch: | 327.2770° |
| orbit number at epoch: | 88667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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